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EFFECTS OF MELTING PRACTICE AND ALUMINUM COATING ON THE LIFE OF GMR 235 BUCKETS OPERATED AT 1650(DEGRE) F IN A TURBOJET ENGINE

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BookPublisher: Nasa, Washington, D.C. 1960Description: 44.DDC classification: NASA | TN D-263

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-263 (Browse shelf)	Not for loan Untraceable		TR15681

Total holds: 0

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Previous	NASA TN D-2607 STABILITY OF FOUR TITANIUM-ALLOY AND FOUR STAINLESS-STEEL SHEET MATERIALS AFTER EXPOSURES UP TO 22000 HOURS AT 550 DEGREE F (560 DEGREE K).	NASA TN D-2608 RADIATION MEASUREMENTS ON THE NINTH MERCURY-ATLAS MISSION (MA-9).	NASA TN D-262 URANIUM DIOXIDE COMPATIBILITY WITH REFRACTORY METALS, CARBIDES, BORIDES, NITRIDES, AND OXIDES BETWEEN 3500(DEGRE ) AND 5000(DEGRE) F	NASA TN D-263 EFFECTS OF MELTING PRACTICE AND ALUMINUM COATING ON THE LIFE OF GMR 235 BUCKETS OPERATED AT 1650(DEGRE) F IN A TURBOJET ENGINE	NASA TN D-2636 - PRELIMINARY INVESTIGATION OF THE HANDLING QUALITIES OF A VEHICLE IN A SIMULATED LUNAR GRAVITATIONAL FIELD	NASA TN D-264 SUITABILITY OF CARBON RESISTORS FOR FIELD MEASUREMENTS OF TEMPERATURES IN THE RANGE OF 35 (DEGRE) TO 100 (DEGRE) R	NASA TN D-265 EXPERIMENTAL RESULTS OF A HEAT-TRANSFER STUDY FROM A FULL-SCALE PEBBLE-BED HEATER	Next

Bound With Nasa Tn D-261-262,264-270

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